Evaluation of a method for computation of separated, turbulent, compressible boundary layers /
M.C. Altstatt.

Description

Main Author

Altstatt, M. C.

Related Names

Arnold Engineering Development Center
United States. Air Force.
ARO, Inc.

Language(s)

English

Published

Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976.

Subjects

Compressibility > Compressibility / Computer programs.
Turbulent boundary layer.

Summary

A computer code for a turbulent, compressible boundary-layer method, capable of carrying out computations in a region of separated flow, is developed and tested. The procedure after separation is to specify either friction velocity or boundary-layer thickness as an independent variable and obtain external velocity as a dependent variable. This requires a trial and error alternation of the specified variable in order to match the desired experimental or computed external velocity. Satisfactorily results were obtained by this method in the analysis of certain specialized cases of separated flow. (Author).

Note

Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.
Final Report: March 21, 1974 -- June 30, 1975."
"February 1976."

Physical Description

44 pages : illustrations ; 28 cm

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